STARLINK-34171, 64082
Orbit data source: Space-Track
STARLINK-34171, 64082 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Wed, 21 May 2025 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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64082 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
USRelated business
Manufacturer
SpaceX/Seattle
Mission
Operational Commercial Communications
Bus & Motor
STARLINK V2MO, Unknown motor
Mass
575 kg wet, ~530 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 17.7 m
Radar Cross Section
36.964 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 19 hours ago
TLE from 19 hours ago
0 STARLINK-34171
1 64082U 25107U 25274.99148102 .00063679 00000-0 22977-2 0 9999
2 64082 42.9995 17.4435 0001702 263.6845 96.3813 15.27664534 21857Epoch: 2025-10-01T23:47Z
TLE epoch observation values (Epoch: 2025-10-01T23:47:43.960Z)
Latitude
0.00001°
Longitude
9.55179°
Altitude
482.701 km
Speed
7.626 km/s
True Right ascension
01h 09m 46s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
12:59:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
485.909 km
Perigee altitude
483.573 km
Semi-major axis
6,862.878 km
Eccentricity
0.00017
Inclination
42.9995°
RAAN
17.4435°
Arg. of periapsis
263.6845°
True anomaly
96.40068°
Mean anomaly
96.3813°
Eccentric anomaly
96.39099°
Mean motion
3.81754 °/min
Orbital period
94.3 mins
BSTAR
0.0022977
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Other satellites on launch #107 in the year 2025 (2025-05-21 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.STARLINK-34171 Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-10-03 08:55:38.288Z | 174.238° S | 2025-10-03 08:57:38.288Z | 140.006° SSE | 14.57° | 2025-10-03 08:59:38.288Z | 107.014° ESE |
| 6 mins | 2025-10-03 10:33:38.288Z | 235.705° WSW | 2025-10-03 10:35:38.288Z | 194.851° SSW | 41.401° | 2025-10-03 10:39:38.288Z | 74.765° E |
| 6 mins | 2025-10-03 12:12:38.288Z | 282.229° WNW | 2025-10-03 12:14:38.288Z | 328.378° NNW | 37.817° | 2025-10-03 12:18:38.288Z | 72.922° E |
| 6 mins | 2025-10-03 13:51:38.288Z | 292.57° NW | 2025-10-03 13:54:38.288Z | 53.546° ENE | 40.769° | 2025-10-03 13:57:38.288Z | 95.094° ESE |
| 5 mins | 2025-10-03 15:30:38.288Z | 270.402° WNW | 2025-10-03 15:32:38.288Z | 226.614° WSW | 31.113° | 2025-10-03 15:35:38.288Z | 146.091° SSE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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